Boeing MD-11F
Service difficulty reports · 31,320
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'MD11F' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'MD11F' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA2019112243029Skin · corrodedNUMEROUS AREAS OF SURFACE CORROSION ON L/H WING UPPER SURFACE XORS-93.00 TO XORS-96.00 STR.17.5 TO STRINGER-19.5...(MRK) REMOVED CORROSION ON L/H WING UPPER SURGACE REF SRM 57-00-01-1A & E.A. #: 1-5730- T0351592 "TITLE: WING - PLATES AND SKINS - LH OUTERSDR FDEA2020012140137Longeron · corrodedAFT CARGO COMPT:CORROSION AT R/H STA 1957 LONGERON 43R DOT NO 4. REMOVED AND REPLACED 48" LONG SECTION OF LONGERON 43 R/H FROM STSA 1948 TO 1997 IAW SRM 53-00-05-2R FIG 201, 202 SHEET 1-3, PG 1-8 DAC DWGS AGA7073, NGA6313.SDR FDEA2019120643181Stiffener · corrodedAFT CARGO TUNNEL:EXFOLIATION AT R/H STA 1960 STRINGER 40 DOT NO 3. REMOVED CORRODED SECTION OF LONGERON AS REQUIRED IAW SRM 53-00-05-2R FIG 202 REPAIR 1 PG 1-8.SDR FDEA2019112243028Skin · corrodedNUMEROUS AREAS 0F SURFACE CORROSION ON L/H WING UPPER SURFACE BETWEEN STA XORS-166.80 TO XORS-201.00/FRONT STR-14 TO STR-19.5....(MRK) REWORKED CORROSION MD-11 SRM 57-00-01-1A SHEET 6SDR FDEA2019112243027Tee Fitting · corrodedAFT CARGO WASTE COMPT:EXFOLIATION AT R/H APX STA 1960 BETWEEN STRINGER 50-51 DOT NO 6. REMOVED AND REPLACED TEE CLIP P/N AGA8002-19 AT STA 1975 BETWEEN R/H L49 AND L/H49 REF SRM 51-35-01, SRM 51-33-01 AND DOUGLAS AGA8002.SDR IPXA2019112049204Bracket · crackedINSPECTION TYPE:2C#3 PYLON WIRE BRIDGE WEB "L" ANGLE IS CRACKED AT TOP, FWD. OF PRECOOLER.REMOVED AND REPLACED BRACKET IAW SRM 54-01-42. (MINOR)SDR IPXA2019111879073Longeron Splice · crackedINSPECTION TYPE:2CCENTER ACCESSORY COMP., LONGERON 37 R/H SPLICE FITTING IS CRACKED AT STA. 6-90.REMOVED, FABRICATED AND REPLACED SPLICE FITTING 37 R/H AT STA. 6-90 IAW DWG. A6A7121 AND SRM 51-33-01. (MINOR)SDR IPXA2019111348980Panel · crackedINSPECTION TYPE:2CRIGHT UNDER WING CANTED PANEL CAP IS CRACKED AT STA. X=1236.8 AND Z=-100.REPAIRED CRACKED RIGHT UNDER WING CANTED PANEL CAP AT STA. X=1236.8 AND Z=-100 IAW UPS EO MD11-5310-74544-A. (MAJOR)SDR FDEA201911042853Hydraulic Line · leakingPDIS 616 29-02 8465 03NOV19 EWR FACT U LOGPAGES:3153051 RECEIVED AT CRUISE "HYD 3 ELEV OFF" ALERT LEV1. QTY HYD 3 WAS 5.9 WELL BELOW CYAN LINE.FOLLOWED QRH.QTY CONTINUED TO DECREASE TO 2.4 THEN AUTO SHUT DOWN. #3 HYD SYSTEM WENT DOWN TO 2.0 SSDR 9WGA2019110401Skin · corrodedCENTER CARGO INTERNAL FUSELAGE SKIN HAS CORROSION AT LONGERON 50L F.S.1621-1721. CENTER CARGO INTERNAL FUSELAGE SKIN HAS CORROSION AT LONGERON 52 F.S. 1561-1601. CENTER CARGO INTERNAL FUSELAGE SKIN HAS CORROSION AT LONGERON 48R F.S.1561-1581. CENTER CARGO INTESDR FDEA201911032849Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-08. OVERSIZED BUSDR FDEA201911032848Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-SDR FDEA201911032847Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-0SDR IPXA2019112249277Door Frame · crackedINSPECTION TYPE:2CMAIN CABIN, L-3 DOOR JAMB INNER SKIN/WEB IS CRACKED AT STA. 1254 AND Z=-13.REPAIRED CRACKED L-3 DOOR JAMB INNER SKIN/WEB AT STA. Y=1254 AND Z=-13 IAW VT-SAA EA 011-5310-01-A7947 REV. I/R AND UPS EO MD11-5310-74635-A. (MAJOR)SDR IPXA2019112049203Support · crackedINSPECTION TYPE:2CR/H O/B FLAP I/B HINGE AFT SIDE FRAME SUPPORT IS CRACKED.REMOVED, FABRICATED AND REPLACED SUPPORT IAW DWG. ARC 2149 AND SRM 51-35-02. (MINOR)SDR FDEA201911032846Doubler · crackedRIGHT WING Ï¿½ FIXED LEADING EDGE RIB DOUBLER AT XOS 667 FOUND CRACK. CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED DOUBLER PER DOUGLAS DRAWING ARB3954 REVISION K.INSTALLED FABRICATED DOUBLER AT RIGHT WING FIXED LEADING EDGE AT XOS 667 AS SDR FDEA201911032845Skin · crackedRIGHT WING Ï¿½ NO. 14 LEADING EDGE SLAT TRACK CUTOUT LOWER SKIN AT XOS 891 FOUND CRACK. REPAIR CARRIED OUT AT RIGHT WING NO. 14 LEADING EDGE SLAT TRACK CUT OUT LOWER SKIN AT XOS 891 AS PER SRM 57-40-02-2R FIGURE 201REPAIR 7. REPAIR CLASSIFIED AS MAJOR PSDR FDEA201911032844Structure · crackedLEFT WING Ï¿½ TRAILING EDGE LOWER SURFACE SILL AT XORS 420 FOUND CRACK. CRACKED SILL REMOVED AS PER SRM 51-34-01-0G AND FABRICATED SILL PER DOUGLAS DRAWING ARC7008 REVISION C. INSTALLED FEBRICATED SILL AT LEFT WING TRAILING EDGE LOWER SURFACE AT XORS 420SDR FDEA201911032843Doubler · crackedLEFT WING Ï¿½ FIXED LEADING EDGE RIB DOUBLER AT XOS 667 FOUND CRACK. CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED DOUBLER PER DOUGLAS DRAWING ARB3954 REVISION K. INSTALLED FABRICATED DOUBLER AT LEFT WING FIXED LEADING EDGE AT XOS 667 AS PSDR FDEA201911032842Doubler · crackedLEFT WING Ï¿½ FIXED LEADING EDGE RIB DOUBLER AT XOS 789 FOUND CRACK. CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED DOUBLER PER DOUGLAS DRAWING ARB3954 REVISION K. INSTALLED FEBRICATED DOUBLER AT LEFT WING FIXED LEADING EDGE AT XOS 789 AS PSDR FDEA201911032841Doubler · crackedLEFT WING Ï¿½ FIXED LEADING EDGE RIB DOUBLER AT XOS 906 FOUND CRACK. CRACKED DOUBLER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED DOUBLER PER DOUGLAS DRAWING ARB3954 REVISION K. INSTALLED FEBRICATED DOUBLER AT LEFT WING FIXED LEADING EDGE AT XOS 906 AS PSDR FDEA201911032840Former · crackedLEFT WING Ï¿½ FIXED LEADING EDGE FORMER AT XOS 584 FOUND CRACK. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED FORMER PER DOUGLAS DRAWING ARB2931 REVISION H. INSTALLED FEBRICATED FORMER AT LEFT WING FIXED LEADING EDGE AT XOS 584 AS PER SRM 5SDR FDEA201911032839Doubler · crackedLEFT WING Ï¿½ FIXED LEADING EDGE BEADED DOUBLER AT XOS 694 FOUND CRACK. REPAIR CARRIED OUT AT LEFT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 694 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201911032834Seat Track · corrodedUPON REMOVAL MAIN DECK DELAMINATED FLOOR PANEL #282JF FOR REPLACEMENT FOUND MAIN DECK FLOOR SEAT TRACK AT STATION 1803 X=-107.25 FLANGE CORRODED. MAIN DECK FLOOR SEAT TRACK FLANGE AT STATION 1803 X=-107.25 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER MDSDR FDEA201911032833Seat Track · corrodedUPON REMOVAL MAIN DECK DELAMINATED FLOOR PANEL #282JF FOR REPLACEMENT FOUND MAIN DECK FLOOR SEAT TRACK AT STATION 1778 X=-107.25 FLANGE CORRODED. MAIN DECK FLOOR SEAT TRACK FLANGE AT STATION 1778 X=-107.25 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER MDSDR FDEA201911032832Seat Track · corrodedUPON REMOVED MAIN DECK DELAMINATED FLOOR PANEL #282JF FOR REPLACEMENT FOUND MAIN DECK FLOOR SEAT TRACK AT STATION 1791 X=-75.25 FLANGE CORRODED. MAIN DECK FLOOR SEAT TRACK AT STATION 1791 X=-75.25 FLANGE CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER MD-1SDR FDEA201911032838Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STATION 1282 X=-47.5 FOUND CROWN DAMAGED. MAIN DECK FLOOR SEAT TRACK CROWN DAMAGED AREA EVALUATED AND FOUND EXCEED LIMIT AS PER MD-11, SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1 AT STATION 1282 X=-47.5. SEAT TRACK REPAIRSDR FDEA201911032837Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STATION 1282 X= 47.5 FOUND CROWN DAMAGED. MAIN DECK FLOOR SEAT TRACK CROWN DAMAGED AT STATION 1282 X= 47.5, CROWN DAMAGED AREA EVALUATED AND FOUND EXCEED LIMIT AS PER MD-11, SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. SESDR FDEA201911032836Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STATION 1391 X= 47.5 FOUND CROWN DAMAGED. MAIN DECK FLOOR SEAT TRACK CROWN DAMAGED AT STATION 1391 X= 47.5.CROWN DAMAGED AREA EVALUATED AND FOUND EXCEED LIMIT AS PER MD11 SRM 53-00-52-1A FIGURE101 ALLOWABLE DAMAGE 1. SEAT SDR FDEA201911032835Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STATION 5-53 X= 47.5 FOUND CROWN DAMAGED. MAIN DECK FLOOR SEAT TRACK CROWN DAMAGED AT STATION 5-53 X= 47.5.CROWN DAMAGED AREA EVALUATED AND FOUND EXCEED LIMIT AS PER MD11 SRM 53-00-52-1A FIGURE101 ALLOWABLE DAMAGE 1. SEATSDR IPXA2019111549009Skin · corrodedINSPECTION TYPE:2CLT WING UPPER SKIN HAS CORROSION BETWEEN STA. XORS =290 AND 298 AT STRINGER 16.REPAIRED CORROSION ON LT WING UPPER SKIN BETWEEN STA. XORS =290 AND 298 AT STRINGER 16 IAW VT-SAA EA 011-5730-01-A7950 REV. IR AND UPS EO MD11-5730-74638-A. (MINORSDR IPXA2019111549008Beam · crackedINSPECTION TYPE:2CFWD CARGO R/H HORIZONTAL BEAM INTERCOSTAL IS CRACKED AT APPROX. STA. 6-70 ABOVE LONGERON 43R.REPAIRED CRACKED FWD CARGO R/H HORIZONTAL BEAM INTERCOSTAL AT APPROX. STA. 6-70 ABOVE LONGERON 43R IAW MD-11 SRM 51-33-01 AND 51-35-01. (MINOR)SDR IPXA2019111549028Tee Fitting · crackedINSPECTION TYPE:2CSTA. 1340, LONGERON 15 L/H TEE ANGLE IS CRACKED.REMOVED, FABRICATED AND REPLACED LONGERON 15 L/H TEE ANGLE AT STA. 1340 IAW DWG. AEA7568 AND SRM 51-35-01. (MINOR)SDR IPXA2019111348977Longeron · crackedINSPECTION TYPE:2CFUSELAGE STA. 1340 LONGERON 15R IS CRACKED.REMOVED AND REPLACED CRACKED LONGERON 15R AT FUSELAGE STA. 1340 IAW MD-11 SRM 51-33-01 & 51-35-01. (MINOR)SDR IPXA2019111348978Intercostal · crackedINSPECTION TYPE:2CFWD, CARGO INTERCOSTAL IS CRACKED BETWEEN STA. 6-30 TO 6-50 AND ABOVE LONG. 43 R/H.REMOVED, FABRICATED AND REPLACED INTERCOSTAL BETWEEN STA. 6.30 TO 6-50 AND ABOVE L43 R/H IAW DWG. ACA7049 AND SRM 51-31-01. (MINOR)SDR IPXA2019111148854Bracket · crackedINSPECTION TYPE:2CR/H O/B FLAP I/B HINGE AFT SIDE ANGLE BRACKET IS GOUGED.REMOVED, FABRICATED AND REPLACED BRACKET IAW DWG. ARC2149 AND SRM 51-31-01. (MINOR)SDR IPXA2019110448594Spring · out of positionINSPECTION TYPE:N/AREF M 688198 L1 DOOR MAIN ENTRY DOOR FLAPPER DOOR SPRING HINGE REPAIR LINKED TO M 688197REPOSITIONED & REINSTALLED FLAPPER DOOR HNGE SPRING ON L1 DOOR REF AMM 20-51-02, IPC 52-11-08-01. OPS CK NORMAL. THIS CLEARS DEFERRAL M 688198SDR IPXA2019110348586Seat Track · crackedINSPECTION TYPE:N/ASEAT TRACK CRACKED AND CORRODED ATSTA 1520 8.50 RREPAIRED PER EO MD11-5310-74517 SEAT TRACK SPLICE REPAIRSDR IPXA2019110348585Seat Track · corrodedINSPECTION TYPE:N/ASEAT TRACK CRACKED AND CORRODED AT STA.1520-8.50LEFTREPAIRED PER EO MD11-5310-74517A SEAT TRACK SPLICE REPAIRSDR FDEA201911022829Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57SDR FDEA201911022828Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE LOWER MOUNT INBOARD HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57- 4SDR FDEA201911022827Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMSDR FDEA201911022826Hinge Bracket · corrodedRIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING - WING SIDE OUTBOARD FLAP INBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57SDR FDEA201911022820Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE LOWER MOUNT OUTBOARD HOLE BORE (#3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57SDR FDEA201911022819Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE PIVOT HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44-09. OVERSIZED BUSHING FABRSDR FDEA201911022818Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT LOWER HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44- 09. SDR FDEA201911022817Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT UPPER HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE BARREL NUT UPPER HOLE BORE (#7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM57-44- 09. SDR FDEA201911022816Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR OUTBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMMSDR FDEA201911022815Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE SURFACE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE(#8 HOLE) SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SDR FDEA201911022814Hinge Bracket · corrodedLEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - WING SIDE OUTBOARD FLAP OUTBOARD HINGE ACTUATOR INBOARD LUG HOLE BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM5
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